Adaptive fault-tolerant spacecraft attitude control using a novel integral terminal sliding mode-Reference-Cited by-同舟云学术

Adaptive fault-tolerant spacecraft attitude control using a novel integral terminal sliding mode

Published:2017-01-16 Issue:16 Volume:27 Page:3174-3196
ISSN:1049-8923
Container-title:International Journal of Robust and Nonlinear Control
language:en
Short-container-title:Int. J. Robust. Nonlinear Control

Author:

Gui Haichao¹,Vukovich George²

Affiliation:

1. Department of Aerospace Engineering; Ryerson University; Toronto Ontario Canada

2. Department of Earth and Space Science and Engineering; York University; Toronto Ontario Canada

Publisher

Wiley

Subject

Electrical and Electronic Engineering,Industrial and Manufacturing Engineering,Mechanical Engineering,Aerospace Engineering,Biomedical Engineering,General Chemical Engineering,Control and Systems Engineering

Reference40 articles.

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2. Inverse optimal adaptive control for attitude tracking of spacecraft;Luo;IEEE Transactions on Automatic Control,2005

3. Robust adaptive variable structure control of spacecraft under control input saturation;Bokovic;Journal of Guidance, Control, and Dynamics,2001

4. Quasi-continuous higher order sliding-mode controllers for spacecraft-attitude-tracking maneuvers;Pukdeboon;IEEE Transactions on Industrial Electronics,2010

5. Attitude tracking of rigid spacecraft with bounded disturbances;Xia;IEEE Transactions on Industrial Electronics,2011

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